SE8402552L - EXHAUST SYSTEM FOR A TURBIN DRIVE FLEX LOADED COMBUSTION ENGINE - Google Patents
EXHAUST SYSTEM FOR A TURBIN DRIVE FLEX LOADED COMBUSTION ENGINEInfo
- Publication number
- SE8402552L SE8402552L SE8402552A SE8402552A SE8402552L SE 8402552 L SE8402552 L SE 8402552L SE 8402552 A SE8402552 A SE 8402552A SE 8402552 A SE8402552 A SE 8402552A SE 8402552 L SE8402552 L SE 8402552L
- Authority
- SE
- Sweden
- Prior art keywords
- exhaust pipe
- combustion engine
- axis
- connecting line
- point
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/02—Gas passages between engine outlet and pump drive, e.g. reservoirs
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Supercharger (AREA)
- Exhaust Silencers (AREA)
Abstract
Exhaust system for an internal combustion engine pressure-charged by a turbo fan, in which the tangent to the connecting line of the centres of gravity of the sections of the ribs of the inlet housing in the planes perpendicular to the axis of the turbine, which planes are indicated in the inlet or outlet cross-section of the rib, is askew in relation to the gas flow direction with the axis of the turbine. The tangent to the connecting line of the centres of gravity of the smallest profile sections of the manifolds 10 is twisted with the axis of the exhaust pipe 7 at the point of the outlet into the exhaust pipe 7 or at the point of the narrowest cross-section of the manifold. The baffle element inserted at the point of connection of branch pipes of the jointed exhaust pipe has at least two vanes.
<??>Each vane is deflected at an angle a from the connecting line of the two adjacent branch pipes of the exhaust pipe within the limits of 15 to 75 degrees.
<IMAGE>
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CS833370A CS242619B1 (en) | 1983-05-13 | 1983-05-13 | Exhaust system of a combustion engine supercharged by turbo blower |
Publications (2)
Publication Number | Publication Date |
---|---|
SE8402552D0 SE8402552D0 (en) | 1984-05-11 |
SE8402552L true SE8402552L (en) | 1984-11-14 |
Family
ID=5373541
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8402552A SE8402552L (en) | 1983-05-13 | 1984-05-11 | EXHAUST SYSTEM FOR A TURBIN DRIVE FLEX LOADED COMBUSTION ENGINE |
Country Status (8)
Country | Link |
---|---|
CS (1) | CS242619B1 (en) |
DE (1) | DE3414537A1 (en) |
DK (1) | DK170184A (en) |
FI (1) | FI841562A (en) |
FR (1) | FR2545875B3 (en) |
NO (1) | NO841907L (en) |
SE (1) | SE8402552L (en) |
SU (1) | SU1390403A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19838703A1 (en) * | 1998-08-26 | 2000-03-02 | Zeuna Staerker Kg | Device for calming the flow in the exhaust pipe of an internal combustion engine |
DE19926349B4 (en) * | 1999-06-10 | 2008-05-15 | Daimler Ag | Exhaust line for large mass flow passing internal combustion engines |
JP4242212B2 (en) * | 2003-06-23 | 2009-03-25 | 株式会社小松製作所 | Turbocharger |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE895677C (en) * | 1941-10-22 | 1953-11-05 | Versuchsanstalt Fuer Luftfahrt | Utilization of the exhaust energy from internal combustion piston engines with a downstream exhaust gas turbine |
DE842873C (en) * | 1950-06-25 | 1952-07-03 | Maschf Augsburg Nuernberg Ag | Exhaust collector for supercharged internal combustion engines with downstream exhaust gas turbine |
CH356959A (en) * | 1957-01-05 | 1961-09-15 | Goetaverken Ab | Internal combustion engine |
CH396517A (en) * | 1962-09-20 | 1965-07-31 | Ledo Dr Carletti | Exhaust pipe system for internal combustion engines |
-
1983
- 1983-05-13 CS CS833370A patent/CS242619B1/en unknown
-
1984
- 1984-03-28 DK DK170184A patent/DK170184A/en not_active IP Right Cessation
- 1984-04-17 DE DE19843414537 patent/DE3414537A1/en not_active Ceased
- 1984-04-18 FI FI841562A patent/FI841562A/en not_active Application Discontinuation
- 1984-04-25 FR FR8406466A patent/FR2545875B3/en not_active Expired
- 1984-05-04 SU SU847773387A patent/SU1390403A1/en active
- 1984-05-11 SE SE8402552A patent/SE8402552L/en not_active Application Discontinuation
- 1984-05-11 NO NO841907A patent/NO841907L/en unknown
Also Published As
Publication number | Publication date |
---|---|
FR2545875B3 (en) | 1985-10-18 |
DK170184A (en) | 1984-11-14 |
CS337083A1 (en) | 1985-08-31 |
NO841907L (en) | 1984-11-14 |
CS242619B1 (en) | 1986-05-15 |
SE8402552D0 (en) | 1984-05-11 |
FI841562A0 (en) | 1984-04-18 |
FR2545875A1 (en) | 1984-11-16 |
DK170184D0 (en) | 1984-03-28 |
DE3414537A1 (en) | 1984-11-15 |
FI841562A (en) | 1984-11-14 |
SU1390403A1 (en) | 1988-04-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NAV | Patent application has lapsed |
Ref document number: 8402552-7 Effective date: 19871201 |